A method and apparatus are provided for controlling a dynamic device having multi inputs and operating in an environment having multiple operating parameters. A method of designing flight control laws using multi-input, multi-output feedback LTI'zation is also provided. The method includes steps of: (i) determining coordinates for flight vehicle equations of motion; (ii) transforming the coordinates for the flight vehicle equations of motion into a multi-input linear time invariant system; (iii) establishing control laws yielding the transformed equations of motion LTI; (iv) adjusting the control laws to obtain a desired closed loop behavior for the controlled system; and (v) converting the transformed coordinates control laws to physical coordinates.
METHOD, APPARATUS AND DESIGN PROCEDURE FOR CONTROLLING MULTI-INPUT, MULTI-OUTPUT (MIMO) PARAMETER DEPENDENT SYSTEMS USING FEEDBACK LTI'ZATION
PROCEDE, APPAREIL ET PROCEDURE DE CONCEPTION PERMETTANT DE CONTROLER DES SYSTEMES DEPENDANT DE PARAMETRES A MULTIPLES ENTREES ET SORTIES, (MIMO) AU MOYEN D'UNE INVARIANCE DE TEMPSLINEAIRE (LTI) DE RETROACTION
2016-02-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung |
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